Abstract
This paper proposes a possible feedback control system for regulating the output voltage and currents of a spacecraft electric power system consisting of parallel fuel-cell modules. Such a control system may be necessary because of the many fuel cell variables that can change the value of the fuel-cell module terminal voltage and cause an unequal division of load between the modules.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
